Ma, Ziqing; Smeur, Ewoud (2022): Wind tunnel data set with a wing at all angles of attack. Version 2. 4TU.ResearchData. dataset. https://doi.org/10.4121/16620226.v2

Version 3 - 2022-07-19 (latest) Version 1 - 2022-01-07

Usage statistics

Categories

• Aerospace Engineering

Keywords

control effectiveness inverse flow tailsitter UAVs wind tunnel test wing-propeller interaction

Geolocation

Time coverage

February 24-26, 2021

Licence

CC0

Export as...

RefWorks BibTeX Reference Manager Endnote DataCite NLM DC CFF

by Ziqing Ma, Ewoud Smeur

This wind tunnel data set was collected at OJF in TU Delft. The aerodynamic forces and moments of a modified MH32 wing at all angles of attack for different flap deflections and 0%, 70% throttle settings are recorded in this data set. This data set should be valuable for the research on tailsitters, especially the impact of inverse flow on the tailsitters in the descending phase.

The repeated experiment data for 0% throttle on Feb 24, 2021 are also provided as a supplement to validate the accuracy of the measurements.

History

• 2022-01-07 first online

• 2022-05-10 published, posted

Publisher

4TU.ResearchData

Format

.txt files for readme and measurements

Organizations

TU Delft, Faculty of Aerospace Engineering